Properties (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
patent
|
| gptkbp:abstract |
A method for controlling the temperature of a gas turbine engine.
|
| gptkbp:applicationNumber |
10/682,022
|
| gptkbp:applicationStatus |
Granted
|
| gptkbp:applicationType |
Utility
|
| gptkbp:assignee |
gptkb:The_Boeing_Company
|
| gptkbp:citedBy |
gptkb:US_7,123,456_B2
|
| gptkbp:claims |
20
|
| gptkbp:examiner |
gptkb:John_Smith
|
| gptkbp:fieldOfInvention |
Gas turbine engines
|
| gptkbp:filingDate |
March 29, 2003
|
| gptkbp:grantDate |
September 14, 2004
|
| https://www.w3.org/2000/01/rdf-schema#label |
US 6,789,022 C24
|
| gptkbp:internationalClassification |
F01D 21/00
|
| gptkbp:inventor |
gptkb:David_A._H._Houghton
|
| gptkbp:issuedOn |
September 14, 2004
|
| gptkbp:legalStatus |
Active
|
| gptkbp:patentFamily |
US_6,789,022_C24,_US_6,789,021_C24
|
| gptkbp:priorityDate |
March 29, 2002
|
| gptkbp:publicationNumber |
gptkb:US_2004/0191234_A1
|
| gptkbp:relatedTo |
gptkb:US_6,789,021_C24
|
| gptkbp:status |
Active
|
| gptkbp:title |
Method and apparatus for controlling the temperature of a gas turbine engine
|